Hey, I was wondering what is the difference between angle of attack and dihedral, from all the videos and Wikipedia sites I have been, they seem to be the exact same thing though I am sure they are not.......so what is the difference? Please don't criticize I am new to this stuff............
@1Abdilatif1 You're in luck! I've covered anhedral/dihedral in the equally exciting video number 10 covering the thrilling world of aircraft stabiity. I warn you now, there is a falling sperm whale in it - please ensure you're adequately prepared for Cetacea genocide. The part you're interested in is at 5:49 (can't link to it because of YouTube anti-spam measures, but go to my channel page and click number 10!). Hope that helps.
LMFAO, I spent 3 hours in a flight school and was so overwhelmed by all the useless info. this is so much more to the point and because it's funny I'm entertained by it. Your better then my instructor! LOL I love the Concorde joke :P
you should study the Aileron Relative to Roll and know the effect over the roll rate after moving the Aileron one degree and study it , then you'll get a relative equation between Roll and Aileron Move.. then you'll know how many degrees you need to move the aileron to gain your desired Roll
Even though Im a girl I wish so badly to be on an airplane someday! Thx for the video, it is great *-*
gokharol 1 week ago
ailerons dont increase AOA, they increase the camber, which increases lift
donnie369369 7 months ago
Hey, I was wondering what is the difference between angle of attack and dihedral, from all the videos and Wikipedia sites I have been, they seem to be the exact same thing though I am sure they are not.......so what is the difference? Please don't criticize I am new to this stuff............
1Abdilatif1 9 months ago
@1Abdilatif1 You're in luck! I've covered anhedral/dihedral in the equally exciting video number 10 covering the thrilling world of aircraft stabiity. I warn you now, there is a falling sperm whale in it - please ensure you're adequately prepared for Cetacea genocide. The part you're interested in is at 5:49 (can't link to it because of YouTube anti-spam measures, but go to my channel page and click number 10!). Hope that helps.
profpilotcouk 9 months ago
Freaking BRILLIANT!!!!!!!!!!!!!!!!
jedoesq 10 months ago
LMFAO, I spent 3 hours in a flight school and was so overwhelmed by all the useless info. this is so much more to the point and because it's funny I'm entertained by it. Your better then my instructor! LOL I love the Concorde joke :P
Daniel7681 1 year ago
U r +Z
53sur 1 year ago
UR THE BESSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSSST TEACHER.....THX ALOT..
sudesh071 1 year ago
u r the best teacher i ever had !!
fly2infiniti 1 year ago
you should go pro
you will do good
keep it up
god bless you
diajassy 1 year ago
"not floating 6 feets to the right of the aircraft" - LOL...thats a good one.
pasirCepat 1 year ago
Oh god I can't keep watching it, its good but if I go and write a test after taking ground school Ill probably burst out laughing
ARandomCanadian 2 years ago
you should study the Aileron Relative to Roll and know the effect over the roll rate after moving the Aileron one degree and study it , then you'll get a relative equation between Roll and Aileron Move.. then you'll know how many degrees you need to move the aileron to gain your desired Roll
cristian07r0nald0 2 years ago
dude, you're a genius! it's not easy to explain things this well. not to mention, hilarious. thanks soooooo much!!!
monalisaofthewolves 2 years ago
I love your videos! they are so useful and nice explained :)
AgnieszkaD1990 2 years ago
how can I calculate the CL in the lift formula ?
with out using the lift formula !
19BlackLord91 2 years ago